国防科技大学学报2017，Vol.39Issue(2)：1-8,8.DOI:10.11887/j.cn.201702001
评估飞控系统的风洞虚拟飞行试验系统与关键技术
Wind tunnel based virtual flight testing system and key technologies for the evaluation of flight control system
摘要
Abstract
In order to provide a guide for specific investigations on WTBVFT(wind tunnel based virtual flight testing) techniques, the test system and key technologies of WTBVFT for the evaluation of FCS (flight control system) were analyzed.Based on the deficiencies of the traditional FCS evaluation methods, the advantages of WTBVFT for evaluation of FCS were analyzed.According to the common constitution of attitude control loop and guidance control loop used by FCS, the test system and working principle of WTBVFT for FCS evaluation were presented.The main differences between the WTBVFT system and the hardware-in-the-loop simulation system were analyzed.The key technologies of WTBVFT for FCS evaluation were also analyzed, including WTBVFT evaluation methods, aircraft model design technique, FCS modification technique, and model support technique.关键词
飞行控制系统评估/风洞虚拟飞行试验/半实物仿真/评估方法/飞行器模型设计/模型支撑Key words
flight control system evaluation/wind tunnel based virtual flight testing/hardware-in-the-loop simulation/evaluation methods/aircraft model design/model support分类
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黄敏,王中伟,郭振云..评估飞控系统的风洞虚拟飞行试验系统与关键技术[J].国防科技大学学报,2017,39(2):1-8,8.基金项目
国家自然科学基金资助项目(51505487) （51505487）
国防科技大学科研计划资助项目(JC15-01-02) （JC15-01-02）
